CA2821142A1 - Compresseur axial - Google Patents

Compresseur axial Download PDF

Info

Publication number
CA2821142A1
CA2821142A1 CA2821142A CA2821142A CA2821142A1 CA 2821142 A1 CA2821142 A1 CA 2821142A1 CA 2821142 A CA2821142 A CA 2821142A CA 2821142 A CA2821142 A CA 2821142A CA 2821142 A1 CA2821142 A1 CA 2821142A1
Authority
CA
Canada
Prior art keywords
guide vane
stage
casing
guide vanes
guide
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CA2821142A
Other languages
English (en)
Other versions
CA2821142C (fr
Inventor
Marco Micheli
Wolfgang Kappis
Luis Federico Puerta
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Ansaldo Energia IP UK Ltd
Original Assignee
Alstom Technology AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Alstom Technology AG filed Critical Alstom Technology AG
Publication of CA2821142A1 publication Critical patent/CA2821142A1/fr
Application granted granted Critical
Publication of CA2821142C publication Critical patent/CA2821142C/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • F01D5/142Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • F01D5/146Shape, i.e. outer, aerodynamic form of blades with tandem configuration, split blades or slotted blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/541Specially adapted for elastic fluid pumps
    • F04D29/542Bladed diffusers
    • F04D29/544Blade shapes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/30Arrangement of components
    • F05D2250/34Arrangement of components translated
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/30Arrangement of components
    • F05D2250/38Arrangement of components angled, e.g. sweep angle

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Geometry (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CA2821142A 2010-12-15 2011-12-07 Compresseur axial Expired - Fee Related CA2821142C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CH02093/10A CH704212A1 (de) 2010-12-15 2010-12-15 Axialkompressor.
CH02093/10 2010-12-15
PCT/EP2011/072052 WO2012080053A1 (fr) 2010-12-15 2011-12-07 Compresseur axial

Publications (2)

Publication Number Publication Date
CA2821142A1 true CA2821142A1 (fr) 2012-06-21
CA2821142C CA2821142C (fr) 2015-11-24

Family

ID=43640279

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2821142A Expired - Fee Related CA2821142C (fr) 2010-12-15 2011-12-07 Compresseur axial

Country Status (11)

Country Link
US (1) US9810226B2 (fr)
EP (1) EP2652337A1 (fr)
JP (1) JP5818908B2 (fr)
CN (1) CN103354875B (fr)
AU (1) AU2011344469B2 (fr)
BR (1) BR112013015252A2 (fr)
CA (1) CA2821142C (fr)
CH (1) CH704212A1 (fr)
MX (1) MX336210B (fr)
RU (1) RU2564386C2 (fr)
WO (1) WO2012080053A1 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2698502A1 (fr) 2012-08-13 2014-02-19 Alstom Technology Ltd Procédé de mesure du jeu à froid des extrémités d'aubes d'une turbomachine et agencement de mesures du jeu des extrémités pour l'exécution de ce procédé
ITMI20130791A1 (it) * 2013-05-14 2014-11-15 Cofimco Srl Ventilatore assiale
FR3019879A1 (fr) * 2014-04-09 2015-10-16 Turbomeca Moteur d'aeronef comprenant un calage azimutal du diffuseur, par rapport a la chambre de combustion
EP3190269A1 (fr) * 2016-01-11 2017-07-12 United Technologies Corporation Étage à sillage de faible énergie
US10502220B2 (en) 2016-07-22 2019-12-10 Solar Turbines Incorporated Method for improving turbine compressor performance
AU2016277549B2 (en) * 2016-10-24 2018-10-18 Intex Holdings Pty Ltd A multi-stage axial flow turbine adapted to operate at low steam temperatures
US20180313364A1 (en) * 2017-04-27 2018-11-01 General Electric Company Compressor apparatus with bleed slot including turning vanes
US11352999B2 (en) * 2018-04-17 2022-06-07 Cummins Filtration Ip, Inc Separation assembly with a two-piece impulse turbine
CN109083849B (zh) * 2018-08-14 2020-06-09 成都市弘盛科技有限公司 一种轴流压气机
WO2023216742A1 (fr) * 2022-05-09 2023-11-16 追觅创新科技(苏州)有限公司 Support de ventilateur, moteur électrique et soufflante

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB628263A (en) * 1943-06-01 1949-08-25 Louis Breguet Improvements in or relating to axial flow compressors
US2798661A (en) * 1954-03-05 1957-07-09 Westinghouse Electric Corp Gas turbine power plant apparatus
US4011028A (en) * 1975-10-16 1977-03-08 Anatoly Nikolaevich Borsuk Axial-flow transsonic compressor
SU1366722A1 (ru) * 1985-04-15 1988-01-15 Университет дружбы народов им.Патриса Лумумбы Двухр дный лопаточный аппарат осевого компрессора
JPS6245397A (ja) 1985-08-23 1987-02-27 Hitachi Plant Eng & Constr Co Ltd 汚水処理装置
JPS6245397U (fr) * 1985-09-06 1987-03-19
US4874289A (en) * 1988-05-26 1989-10-17 United States Of America As Represented By The Secretary Of The Air Force Variable stator vane assembly for a rotary turbine engine
US4981414A (en) * 1988-05-27 1991-01-01 Sheets Herman E Method and apparatus for producing fluid pressure and controlling boundary layer
EP1674734A1 (fr) * 2004-12-21 2006-06-28 ALSTOM Technology Ltd Méthode d' amélioration de la stabilité de courant d' une turbomachine
EP2194234A1 (fr) * 2008-12-03 2010-06-09 Siemens Aktiengesellschaft Anneau d'isolation thermique pour contrôle passif de jeu dans une turbine à gaz
US8087249B2 (en) * 2008-12-23 2012-01-03 General Electric Company Turbine cooling air from a centrifugal compressor
EP2218876A1 (fr) * 2009-02-16 2010-08-18 Siemens Aktiengesellschaft Bague d'étanchéité destinée à rendre étanche un jeu radial dans une turbine à gaz
DE102009013399A1 (de) 2009-03-16 2010-09-23 Mtu Aero Engines Gmbh Tandemschaufelkonstruktion
DE102009023100A1 (de) * 2009-05-28 2010-12-02 Rolls-Royce Deutschland Ltd & Co Kg Strömungsmaschine mit einer Schaufelreihengruppe mit meridionalem Kantenabstand

Also Published As

Publication number Publication date
AU2011344469A1 (en) 2013-07-11
WO2012080053A1 (fr) 2012-06-21
CN103354875B (zh) 2016-08-24
EP2652337A1 (fr) 2013-10-23
US20130280053A1 (en) 2013-10-24
US9810226B2 (en) 2017-11-07
CH704212A1 (de) 2012-06-15
BR112013015252A2 (pt) 2016-09-13
CA2821142C (fr) 2015-11-24
RU2013132197A (ru) 2015-01-20
AU2011344469B2 (en) 2015-06-25
JP2014503736A (ja) 2014-02-13
CN103354875A (zh) 2013-10-16
MX2013006789A (es) 2013-10-01
RU2564386C2 (ru) 2015-09-27
JP5818908B2 (ja) 2015-11-18
MX336210B (es) 2016-01-11

Similar Documents

Publication Publication Date Title
CA2821142C (fr) Compresseur axial
RU2293221C2 (ru) Рециркуляционная структура для турбокомпрессора, авиационный двигатель и стационарная турбина, имеющие турбокомпрессор с такой рециркуляционной структурой
RU2586426C2 (ru) Статор осевой турбомашины с элеронами в хвостовиках лопаток
US7186072B2 (en) Recirculation structure for a turbocompressor
US9476315B2 (en) Axial flow turbine
US9963973B2 (en) Blading
KR102196815B1 (ko) 베인을 갖는 반경류 또는 혼류 압축기 디퓨저
EP2096262A1 (fr) Turbine à flux axial avec des pertes de fuites réduites
WO2015019901A1 (fr) Compresseur centrifuge et compresseur d'alimentation
US20120224955A1 (en) Diffuser
US20110311355A1 (en) Axial turbo compressor for a gas turbine having low radial gap losses and diffuser losses
KR20170026493A (ko) 방사상 컴프레서용 디퓨저
JP2016539276A (ja) 遠心圧縮機の湾曲した拡散流路部
US11781442B2 (en) Turbine having an internal secondary space equipped with fins for correcting gyration of an airflow
US11047246B2 (en) Blade or vane, blade or vane segment and assembly for a turbomachine, and turbomachine
EP2649279B1 (fr) Machine à écoulement de fluide, en particulier turbine à gaz pénétrée axialement par un écoulement de gaz chaud
KR102569738B1 (ko) 래디얼 압축기용 디퓨저
US20130136619A1 (en) Blading
US10041352B2 (en) Stator of a turbine of a gas turbine with improved cooling air routing
US8322972B2 (en) Steampath flow separation reduction system
JP2018135836A (ja) 遠心圧縮機
US20060051200A1 (en) Flow structure for a gas turbine
RU2728550C1 (ru) Устройство отбора воздуха в роторе компрессора турбореактивного двигателя
US20250003347A1 (en) High-pressure gas turbine for turbomachine and turbomachine
RU2303140C1 (ru) Турбинная ступень

Legal Events

Date Code Title Description
EEER Examination request

Effective date: 20131230

MKLA Lapsed

Effective date: 20191209